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1. 发明申请

WO2014197089A9 MODULATED TURBINE COOLING SYSTEM 审中-公开
标题翻译：调制涡轮冷却系统
公开(公告)号：WO2014197089A9
公开(公告)日：2015-03-19
申请号：PCT/US2014028673
申请日：2014-03-14
申请人： GEN ELECTRIC
发明人： RAHAIM JOHN JOSEPH , FUSINATO DANIEL JOHN , HUNTER SCOTT DAVID , KIRK JOEL FRANCIS , MELZAK MICHAEL ROBERT , STOVER CURTIS WALTON
IPC分类号： F01D5/08 , F02C7/12
CPC分类号： F01D25/12 , F01D5/02 , F01D5/082 , F01D25/14 , F02C7/125 , F05D2220/32 , F05D2240/24 , F05D2260/20 , F05D2270/3062 , F05D2270/62 , Y02T50/676
摘要： A flow transfer apparatus for transferring cooling flow from a primary gas flowpath (P) to a turbine rotor (128). The apparatus includes: a first supply plenum (92) communicating with the primary gas flowpath (P) and first inducers (148 A), the first inducers (148 A) configured to accelerate a first fluid flow from the first supply plenum (92) and discharge it toward the rotor with a tangential velocity; a second supply plenum (96) communicating with the primary gas flowpath (P) and second inducers (148B), the second inducers (148B) configured to accelerate a second fluid flow from the second supply plenum (96) towards the rotor with a tangential velocity; and a cooling modulation valve (98) operable to selectively permit or block the second fluid flow from the primary gas flowpath (P) to the second supply plenum (96). The valve includes a flow control structure (108, 110) disposed in the primary gas flowpath (P) and an actuation structure extending to a location radially outside of a casing (76) defining the primary gas flowpath (P).
摘要翻译：一种用于将冷却流从主气体流动路径（P）传递到涡轮机转子（128）的流动传递装置。该装置包括：与主气体流路（P）和第一诱导器（148A）连通的第一供应气室（92），第一诱导器（148A）配置成加速来自第一供应气室（92）的第一流体流，并以切向速度朝转子排出; 与主气体流路（P）和第二诱导器（148B）连通的第二供应气室（96），所述第二诱导器（148B）被配置为利用切向方向将来自第二供应气室（96）的第二流体流加速到转子速度; 和可操作以选择性地允许或阻挡从主气体流动路径（P）到第二供应增压室（96）的第二流体流的冷却调节阀（98）。阀包括布置在主气体流动路径（P）中的流动控制结构（108,110）和延伸到限定主气体流动路径（P）的壳体（76）的径向外侧的位置的致动结构。

2. 发明申请

WO2016032585A2 TURBINE ENGINE, COMPONENTS, AND METHODS OF COOLING SAME 审中-公开
标题翻译：涡轮发动机，组件和冷却方法
公开(公告)号：WO2016032585A2
公开(公告)日：2016-03-03
申请号：PCT/US2015032855
申请日：2015-05-28
申请人： GEN ELECTRIC
发明人： MANNING ROBERT FRANCIS , STONE TIMOTHY DERYCK , BUHLER JARED PETER , CORRELA VICTOR HUGO SILVA , LASKOWSKI GREGORY MICHAEL , MURRAY ROBERT CARL , PROCTOR ROBERT , RATZLAFF JONATHAN RUSSELL , S JOHN HOWARD , STOVER CURTIS WALTON
IPC分类号： F02C7/052
CPC分类号： F01D25/32 , B01D45/16 , B04C3/00 , B04C3/06 , B04C2003/003 , B04C2003/006 , F01D5/08 , F01D25/12 , F02C3/04 , F02C7/05 , F02C7/052 , F02C7/18 , F02C9/18 , F05D2220/32 , F05D2240/35
摘要： A centrifugal separator for removing particles from a fluid stream includes an angular velocity increaser configured to increase the angular velocity of a fluid stream, a flow splitter configured to split the fluid stream to form a concentrated-particle stream and a reduced-particle stream, and an exit conduit configured to receive the reduced-particle stream. An inducer assembly for a turbine engine includes an inducer with a flow passage having an inducer inlet and an inducer outlet in fluid communication with a turbine section of the engine, and a particle separator, which includes a particle concentrator that receives a compressed stream from a compressor section of the engine and a flow splitter. A turbine engine includes a cooling air flow circuit which supplies a fluid stream to a turbine section of the engine for cooling, a particle separator located within the cooling air flow circuit, and an inducer forming a portion of the cooling air flow circuit in fluid communication with the particle separator. A method of cooling a rotating blade of a turbine engine having an inducer includes directing a cooling fluid stream from a portion of turbine engine toward the rotating blade, separating particles from the cooling fluid stream by passing the cooling fluid stream through a inertial separator, accelerating a reduced- particle stream emitted from the inertial separator to the speed of the rotating blade, and orienting the reduced-particle stream by emitting the reduced-particle stream from the inertial separator into a cooling passage in the inducer.
摘要翻译：用于从流体流中去除颗粒的离心分离器包括配置成增加流体流的角速度的角速度增加器，配置成分离流体流以形成浓缩颗粒流和减少颗粒流的分流器，以及出口导管，其被配置为接收减少的颗粒流。用于涡轮发动机的诱导器组件包括具有流道的诱导器，所述诱导器具有与发动机的涡轮段流体连通的诱导器入口和诱导器出口以及包括颗粒分离器的颗粒分离器，所述颗粒分离器接收来自发动机的压缩机部分和分流器。涡轮发动机包括冷却空气流动回路，该冷却空气流动回路将流体流供应到发动机的涡轮部分以用于冷却，位于冷却空气流动回路内的颗粒分离器以及形成流体连通的冷却空气流动回路的一部分的诱导器与粒子分离器。一种冷却具有诱导轮的涡轮发动机的旋转叶片的方法包括：引导来自涡轮发动机的一部分的冷却流体流朝向旋转叶片，通过使冷却流体流经过惯性分离器而从冷却流体流中分离出粒子，从惯性分离器释放的减少的颗粒流到旋转叶片的速度，并且通过将来自惯性分离器的减少的颗粒流释放到诱导器中的冷却通道中来定向减少的颗粒流。

3. 发明申请

WO2014197089A2 MODULATED TURBINE COOLING SYSTEM 审中-公开
标题翻译：调节式涡轮冷却系统
公开(公告)号：WO2014197089A2
公开(公告)日：2014-12-11
申请号：PCT/US2014028673
申请日：2014-03-14
申请人： GEN ELECTRIC
发明人： RAHAIM JOHN JOSEPH , FUSINATO DANIEL JOHN , HUNTER SCOTT DAVID , KIRK JOEL FRANCIS , MELZAK MICHAEL ROBERT , STOVER CURTIS WALTON
IPC分类号： F02C3/14
CPC分类号： F01D25/12 , F01D5/02 , F01D5/082 , F01D25/14 , F02C7/125 , F05D2220/32 , F05D2240/24 , F05D2260/20 , F05D2270/3062 , F05D2270/62 , Y02T50/676
摘要： A flow transfer apparatus for transferring cooling flow from a primary gas flowpath (P) to a turbine rotor (128). The apparatus includes: a first supply plenum (92) communicating with the primary gas flowpath (P) and first inducers (148 A), the first inducers (148 A) configured to accelerate a first fluid flow from the first supply plenum (92) and discharge it toward the rotor with a tangential velocity; a second supply plenum (96) communicating with the primary gas flowpath (P) and second inducers (148B), the second inducers (148B) configured to accelerate a second fluid flow from the second supply plenum (96) towards the rotor with a tangential velocity; and a cooling modulation valve (98) operable to selectively permit or block the second fluid flow from the primary gas flowpath (P) to the second supply plenum (96). The valve includes a flow control structure (108, 110) disposed in the primary gas flowpath (P) and an actuation structure extending to a location radially outside of a casing (76) defining the primary gas flowpath (P).
摘要翻译：一种用于将冷却流从初级气体流路（P）传递到涡轮机转子（128）的流动传递装置。该设备包括：与初级气体流路（P）和第一诱导器（148A）连通的第一供应气室（92），构造成加速来自第一供气室（92）的第一流体流的第一诱导器（148A）并以切向速度向转子排放; 与主要气体流路（P）和第二诱导器（148B）连通的第二供应压力室（96），所述第二诱导器（148B）被配置为加速来自第二供应压力室（96）的第二流体流向切向的转子速度; 以及冷却调节阀（98），其可操作以选择性地允许或阻挡来自所述主气流路径（P）到所述第二供气室（96）的所述第二流体流。阀包括设置在主气流路径（P）中的流量控制结构（108,110）和延伸到限定主气流径（P）的壳体（76）径向外侧的位置的致动结构。

4. 发明申请

WO2016099662A3 IMPINGEMENT COOLED TURBINE ENGINE COMPONENT 审中-公开
标题翻译：涡流冷却涡轮发动机部件
公开(公告)号：WO2016099662A3
公开(公告)日：2016-07-21
申请号：PCT/US2015057708
申请日：2015-10-28
申请人： GEN ELECTRIC
发明人： BERGHOLZ ROBERT FREDERICK , ALLEN JASON RANDOLPH , BRIGGS ROBERT DAVID , FELDMANN KEVIN ROBERT , STOVER CURTIS WALTON , WEBSTER ZACHARY DANIEL , REITER FERNANDO
IPC分类号： F01D5/18
CPC分类号： F01D25/12 , F01D5/187 , F01D5/188 , F01D9/041 , F01D11/08 , F02C3/04 , F02C7/18 , F05D2220/32 , F05D2240/127 , F05D2240/128 , F05D2240/24 , F05D2240/35 , F05D2250/38 , F05D2250/712 , F05D2260/201 , F05D2260/202 , F05D2260/2212 , F05D2260/22141 , F05D2260/607 , F23R3/002 , F23R3/005 , F23R3/04 , F23R3/06 , F23R2900/03042 , F23R2900/03044 , F23R2900/03045 , Y02T50/672 , Y02T50/673 , Y02T50/676
摘要： An engine component assembly includes a first engine component having a hot surface in thermal communication with a hot combustion gas flow and a cooling surface with at least one cavity. A second engine component is spaced from the cooling surface, and includes at least one cooling aperture. The cooling aperture is arranged such that cooling fluid impinges on the cooling surface at an angle.
摘要翻译：发动机部件组件包括具有热表面与热燃烧气流热连通的第一发动机部件和具有至少一个腔的冷却表面。第二发动机部件与冷却表面间隔开，并且包括至少一个冷却孔。冷却孔被布置成使得冷却流体以一定角度撞击在冷却表面上。

5. 发明申请

WO2016025054A3 ENGINE COMPONENTS WITH IMPINGEMENT COOLING FEATURES 审中-公开
标题翻译：发动机组件与冲击冷却功能
公开(公告)号：WO2016025054A3
公开(公告)日：2016-04-07
申请号：PCT/US2015032597
申请日：2015-05-27
申请人： GEN ELECTRIC
发明人： STOVER CURTIS WALTON , RAUSCH JONATHAN MICHAEL , ATSUCHI SATOSHI , BRAINCH GULCHARAN SINGH , BRIGGS ROBERT DAVID , BUNKER RONALD SCOTT , KULKARNI AMBARISH JAYANT , MEADE MICHAEL ALAN , PRITCHARD BYRON ANDREW , PROCTOR ROBERT
IPC分类号： F01D5/18
CPC分类号： F02C7/18 , F01D5/189 , F01D9/041 , F01D11/08 , F01D25/12 , F05D2240/81 , F05D2250/38 , F05D2260/201 , F05D2260/202 , F05D2260/22141 , F05D2260/607 , F23R3/002 , F23R3/005 , F23R2900/03042 , F23R2900/03043 , F23R2900/03044 , F23R2900/03045 , Y02T50/673 , Y02T50/676
摘要： Gas turbine engine components are provided which utilize an insert to provide cooling air along a cooled surface of an engine component. The insert provides an array of cooling holes or apertures which are facing the cool side surface of the engine component and direct cooling air onto that cool side surface. The apertures may be formed in arrays and are directed at an oblique angle or a non-orthogonal angle to the surface of the insert and further may be at an angle to the surface of the engine component being cooled. An engine component assembly is provided with counterflow impingement cooling. The engine component comprises an engine component cooling surface having a cooling fluid flow path on one side thereof and a second component adjacent to the first component. The second component, for example an insert, may have a plurality of openings forming an array wherein the openings extend through the second component at a non-orthogonal angle to the surface of the second component. The array of openings create counterflows in substantially opposite directions along the engine component cooling surface.
摘要翻译：提供燃气涡轮发动机部件，其利用插入件沿发动机部件的冷却表面提供冷却空气。插入件提供了一组面向发动机部件的冷却侧表面的冷却孔或孔，并将冷却空气直接冷却到该冷却侧表面上。孔可以形成为阵列并且以与插入件的表面成倾斜的角度或非正交的角度定向，并且还可以与被冷却的发动机部件的表面成一角度。发动机部件组件设有逆流冲击冷却。发动机部件包括在其一侧具有冷却流体流动路径的发动机部件冷却表面和与第一部件相邻的第二部件。第二部件，例如插入件，可以具有形成阵列的多个开口，其中开口以与第二部件的表面成非正交角延伸穿过第二部件。开口阵列沿着发动机部件冷却表面沿基本上相反的方向产生逆流。

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